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Meshing profile 2D

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Hi,

I am working on a 2D wing simulation. I drew a convexe profile and I want to mesh it before computing a tuburlent flow SST phyisic. I have troubles with my solutions convergence and I think it is because of my mesh. I followed the tutorial "flow around an inclined NACA" but I need a more precise mesh for my profile. I tried to make it finer but it didn't work. That is why I want to sudivide my profil to make different domains (by adding points ?) like in the attached file.

Do you think it will resolve my problem ? How can I do such sbidivisions along my profil ?

Thank you,

Best regards,

Julien



0 Replies Last Post 2018年3月18日 GMT-4 14:09
COMSOL Moderator

Hello Julien Gordon

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